European Academy of Parachute Rigging e.V - Luitpoldstr. 30 - D87700 Memmingen - Germany Under approval of EPTA European Paraglider Testlaboratory Alicane
7. Roll stability and damping – 4.4.7 / 2.3.2 Oscillations Roll dampening 8. Stability in gentle spirals 4.4.8 Tendency to return to straight flight 9. Behaviour in a steeply banked turn – 4.4.9 Sink rate after two turns
Flight Test-Report
Rev. 1.0
Stand - 10.01.2008 Seite 1
10. Symmetric front collapse – 4.4.10 / 2.3.5 trim speed
Entry Travel Recovery
accelerated
Dive forward angle on exit Cascade occurs Entry Travel
Rocking back less than 45° > 10 cm
A
1 1
Rocking back less than 45° > 10 cm
Spontaneous in 3 to 5 sec
B
1-2
Spontaneous in 3 to 5 sec
B
1-2
60° - 90° Keeping course No Rocking back less than 45° > 10 cm
D A A
2-3 1 1 1
60° - 90° Entering a turn of less than 90° No Rocking back greater than 45° > 10 cm Recovery through pilot action in less than a further 3 sec 60° - 90° Entering a turn of less than 90° No
D A C
2-3 1 2 1
Spontaneous in 3 to 5 sec
B
1-2
60° - 90° No
D A
2-3 1
Recovery
NA
Dive forward angle on excit Change of course Cascade occurs
NA NA NA
Recovery Dive forward angle on exit Cascade occurs
Keeping course
A
1 1
D
2-3
D A
2-3 1
NA
NA
NA
NA NA NA
NA NA NA
NA NA NA
11. Exiting deep stall (parachutal stall) – 4.4.11 / 2.3.4 Deep stall achieved
No
No
12. High angle of attack recovery – 4.4.12 Recovery
Spontaneous in less than 3 sec
A
Spontaneous in less than 3 sec
A
Cascade occurs
No
A
No
A
bumpy 30° to 60° No collapse No Less than 45° Most lines tight
B A A A A
13. Recovery from a develoved full stall – 4.4.13 / 2.3.8 Behavior after initation Dive forward angle on exit Collapse Cascade occurs (other than collapse) Rocking back Line tension
bumpy 30° to 60° No collapse No Less than 45° Most lines tight
B A A A A
2 1 1 1 1 1
2 1 1 1 1 1
Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs Turn rate Altitude loss Stabilisation Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs Turn rate Altitude loss Stabilisation Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs Turn rate Altitude loss Stabilisation Change of course until re-inflation Re-inflation behavior Total change of course Collapse on the opposite side occurs Twist occurs Cascade occurs
with 75% collapse-Maximum dive forward or roll angle
Re-inflation behavior
with 50% collapse and accelerator-Maximum dive forward or roll angle
Change of course until re-inflation
with 75% collapse and accelerator-Maximum dive forward or roll angle
Turn rate Altitude loss Stabilisation
with 50% collapse-Maximum dive forward or roll angle
14. Asymmetric collapse – 4.4.14 / 2.3.6 Average Low Independent Less than 90°
1-2 1 1 Dive or roll angle
15° to 45°
A
1
Average Avarage Independent Less than 90°
1-2 1-2 1 Dive or roll angle
15° to 45°
A
1
Spontaneous re-inflation
A
1
Spontaneous re-inflation
A
1
Less than 360° No No No Average Avarage Independent
A A A A
1 1 1 1 1-2 1-2 1
Less than 360° No No No Average Avarage Independent
A A A A
1 1 1 1 1-2 1-2 1
C
2
180° to 360°
C
2
Inflates in less than 3 sec from start of pilot action
C
2
Inflates in less than 3 sec from start of pilot action
C
2
Less than 360° No No No
A A A A
1 1 1 1
Less than 360° Yes, no turn reversal No No
A C A A
1 2 1 1
90° to 180°
Dive or roll angle
45° to 60°
Average Avarage Independent 90° to 180°
1-2 1-2 1 Dive or roll angle
45° to 60°
Spontaneous re-inflation
C
2
A
1
Dive or roll angle
15° to 45°
High Avarage Independent
2-3 1-2 1 B
1-2
Spontaneous re-inflation
A
1
A A A A
1 1 1 1 2-3 2 1
C
2
90° to 180°
Dive or roll angle
15° to 45°
A A A A
1 1 1 1 2-3 2 1
Less than 360° No No No High High Independent
C
2
180° to 360°
Inflates in less than 3 sec from start of pilot action
C
2
Inflates in less than 3 sec from start of pilot action
C
2
Less than 360° No No No
A A A A
1 1 1 1
Less than 360° Yes, no turn reversal No No
A C A A
1 2 1 1
Less than 360° No No No High High Independent 90° to 180°
Dive or roll angle 60° to 90°
Dive or roll angle
15° to 45°
15. Directional control with a maintained asymmetric collapse – 4.4.15 / 2.3.7 Able to keep course 180° turn away from the collapsed side possible in 10 sec Amount of control range between turn and stall or spin Counter turn
Yes
A
1
Yes
A
1
Yes
A
1
Yes
A
1
25% to 50% of the symmetric control travel
C
2
25% to 50% of the symmetric control travel
C
2
1
Simple without tendency to stall
1 1 1 1
No No No Non existing
1
Up to 90°
Simple without tendency to stall
1
16. Trim speed spin tendency - 4.4.16 / 2.3.3 & 2.3.11 Spin occurs Asymmetric collapse Front collapse Spin tendency
No No No Non existing
Dive forward
Up to 90°
Flight Test-Report
A
Rev. 1.0
A
1 1 1 1 1
Stand - 10.01.2008 Seite 2
17. Low speed spin tendency - 4.4.17 Spin occurs
No
A
No
A
18. Recovery from a developed spin – 4.4.18 / 2.3.10 Spin rotation angle after release
Stops spinning in less than 90°
A
1
Stops spinning in less than 90°
A
1
Cascade occurs
No
A
1
No
A
1
Initiation Change of course before release
Easy Changing less than 45°
A
1 1
Easy Changing less than 45°
A
1 1
Behaviour before release
Remains stable with straight span
A
1
Remains stable with straight span
A
1
Reocvery
Spontaneous in 3 sec to 5 sec
B
1-2
Spontaneous in less than 3 sec
A
1
Dive forward angle on exit Cascade occurs
0° to 30° No
A A
1 1
0° to 30° No
A A
1 1
Entry procedure
Standard technique
A
1
Standard technique
A
1
Behaviour during big ears
Stable flight Recovery through pilot action in less than a further 3 sec 0° to 30°
A
1
A
1
B
1-2
B
1-2
A
1
Stable flight Recovery through pilot action in less than a further 3 sec 0° to 30°
A
1
19. B-line-stall – 4.4.19 / 2.3.13
20. Big ears – 4.4.20 / 2.3.9
Recovery Dive forward angle on exit 21. Big Ears in accelerated flight – 4.4.21 / 2.3.9 Entry procedure
Standard technique
A
1
Standard technique
A
1
Behaviour during big ears
Stable flight Recovery through pilot action in less than a further 3 sec 0° to 30°
A
1
A
1
B
1-2
B
1-2
A
1
Stable flight Recovery through pilot action in less than a further 3 sec 0° to 30°
A
1
Stable flight
A
1
Stable flight
A
1
Initation Tendency to return straight flight
Average Spontaneous exit
A
1-2 1
Average Spontaneous exit
A
1-2 1
Turn angle to recover normal flight
720° to 1080°, spontaneous recovery
C
2
720° to 1080°, spontaneous recovery
C
2
Recovery Dive forward angle on exit Behaviour immediately after releasing the accelarator while maintaining big ears 22. Behaviour exiting a steep spiral 4.4.22 – 2.3.12
16 m/s
Sink rate when evaluating spiral stability
15 m/s
23. Alternative means of directional control – 4.4.23 / 2.3.3 180° turn achievable in 20 sec
Yes
Stall or spin occurs
No
A A
1
Yes
A
1
1
No
A
1
24. Any other flight procedure and/or configuration described in the user's manual Procedure works as descibed Procedure suitable for novice pilots Cascade occurs Remarks of Test pilot:
NA NA NA 0 0 0 0 0
Copyright Ralf Antz 2008
Flight Test-Report
NA NA NA 0 0 0 0 0
This Flight Test Report ist valid without subscription
oder Anderer zu Verletzungen führen. Die Montage des Rollers muss durch. Erwachsene erfolgen. Der Roller ist für Kinder bis zu 20 kg konzipiert. Bitte heben.
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